08/31/2021Patrick Standish
Installing new inspection holes, modifying the wing tip fairings, and inspecting the wing spars for intergranular corrosion.
08/31/2021Patrick Standish
Inspecting the existing aluminum vertical stabilizer forward attach fitting for cracks, and replacing any cracked parts.
08/31/2021Patrick Standish
How to preclude failure of the exhaust stacks which can cause carbon monoxide contamination of the cabin when cabin heat is used.
08/31/2021Patrick Standish
Remove the fairing at the wing root of each wing and inspect the wing root area for interference between the forward fuel line and the aileron cable and/or aileron pulley.
08/31/2021Patrick Standish
Extreme surface corrosion has been found to exist inside the fuselage spar carry through structures of Luscombe Series 8 aircraft, particularly in those airplanes located near coastal areas.
08/31/2021Patrick Standish
Due to recurring failures of the control cables, all cables should be carefully inspected at each section which passes either over a pulley or through a fairlead.
08/31/2021Patrick Standish
Luscombe equipped with carburetor engines and fuselage fuel tanks without appropriate modifications to the fuel system may experience engine failure during takeoff and climb under low fuel conditions.
08/31/2021Patrick Standish
Inspect for crushing of the stabilizer front spar and the aluminum alloy reinforcing spacers.
08/31/2021Patrick Standish
Inspect the vertical stabilizer rear spar fuselage attachment fitting for evidence of cracks in the fitting flange.
08/31/2021Patrick Standish
Remove small baffle LAC P/N 181112 to allow for more accurate airspeed readings. With baffle installed readings can be incorrect by as much as +15 mph.
08/31/2021Patrick Standish
Remove the tires and inspect the wheel flanges for fatigue cracks.
08/31/2021Patrick Standish
Inspect all seaplanes to determine if the bulkhead reinforcements of Luscombe Drawing 48701 are presently installed at fuselage Station 4.
08/31/2021Patrick Standish
Determine if the attachment of the rudder control arm to the torque tube has been reinforced by a steel strap.
08/31/2021Patrick Standish
Replace the adjustment screw in the lower end of the control stick horn, with an AN 520-10-44 screw in order to prevent interference with the lower fuselage skin.